Novel cross flapping wing aircraft
The utility model provides a novel cross flapping wing aircraft, its characterized in that: it includes four wings, and the cross flapping wings are formed to four wings, and every wing all adopts slider-crank mechanism, and every wing includes pendulum rod, crank, frame, one-level reducing gear, mo...
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Format: | Patent |
Sprache: | eng |
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Zusammenfassung: | The utility model provides a novel cross flapping wing aircraft, its characterized in that: it includes four wings, and the cross flapping wings are formed to four wings, and every wing all adopts slider-crank mechanism, and every wing includes pendulum rod, crank, frame, one-level reducing gear, motor, first bearing, second bearing, one-level reducing gear includes first gear and second gear. The utility model discloses utilize modified slider-crank structure to realize that fluttering of wing provides lift, and become cross symmetrical arrangement for the multi-direction flight of every single move roll all around can be realized to the flapping wing aircraft, and can realize the function of hovering. |
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